| 波音737—200／300／500飞机尾部结构疲劳裂纹的探伤检查 |
| |
| 引用本文： | 唐健,聂有传.波音737—200／300／500飞机尾部结构疲劳裂纹的探伤检查[J].南昌航空工业学院学报,1998(3):74-77. |
| |
| 作者姓名： | 唐健 聂有传 |
| |
| 作者单位： | [1]南方航空（集团）公司维修 [2]广州飞机维修工程公司 |
| |
| 摘 要： | 波音系列飞机一定时间后，飞机尾部结构出现疲劳裂纹，需用涡轮检测法进行损伤检查。
|
| 关 键 词： | 探伤 疲劳裂纹 涡流检验 飞机 机尾 |
The Flaw Inspection of Fatique craacks in the Tail structure of Boeing 737 200/300/500 Aircrafts |
| |
| Tang Jian.The Flaw Inspection of Fatique craacks in the Tail structure of Boeing 737 200/300/500 Aircrafts[J].Journal of Nanchang Institute of Aeronautical Technology(Natural Science Edition),1998(3):74-77. |
| |
| Authors: | Tang Jian |
| |
| Institution: | Tang Jian (Maintaining plant of South Aviation Corporation) Nie Youchuan (Guang Zhou aircraft maintaining company) |
| |
| Abstract: | After a period of time, the fatique crack will appear in the tail structure of Boeing serials aircrafts. It is necessary to use Vortex Detection to inspect this kind of flaw. |
| |
| Keywords: | flaw detection fatigue crack eddy current testing boeing aircraft |
| 本文献已被 CNKI 维普 等数据库收录！ |
